A successful brazing process was developed and evaluated for fabricating full-scale titanium-clad Borsic/aluminum skin-stringer panels. A panel design was developed consisting of a hybrid composite skin reinforced with capped honeycomb-core stringers. Six panels were fabricated for inclusion in the program which included laboratory testing of panels at ambient temperatures and 533 K (500 F) and flight service evaluation on the NASA Mach 3 YF-12 airplane. All panels tested met or exceeded stringent design requirements and no deleterious effects on panel properties were detected followng flight service evaluation on the YF-12 airplane.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Fabrication and evaluation of brazed titanium-clad borsic/aluminum skin-stringer panels


    Beteiligte:
    Bales, T. T. (Autor:in) / Royster, D. M. (Autor:in) / Mcwithey, R. R. (Autor:in)

    Erscheinungsdatum :

    01.07.1980


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Brazed Borsic/aluminum structural panels

    Bales, T. T. / Wiant, H. R. / Royster, D. M. | NTRS | 1977


    Brazed Borsic/Aluminum Structural Panels

    T. T. Bales / H. R. Wiant / D. M. Royster | NTIS | 1977